Reverse core turbine engine mounted above aircraft wing
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United States of America Patent
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Feb 12, 2019
Grant Date -
Oct 22, 2015
app pub date -
Mar 4, 2013
filing date -
Nov 12, 2012
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Abstract
A gas turbine engine has a fan inlet and a fan configured to deliver air to an exhaust nozzle. A core gas turbine engine. including in serial order extending further into the engine, a core turbine section, a combustor and a core compressor section. A core engine inlet duct is spaced from the fan inlet. A method is also described.
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